sxt soft x-ray telescope onboard the yohkoh satellite sxt.ppt
TRANSCRIPT
SXT
Soft X-Ray TelescopeOnboard theYohkoh Satellitehttp://solar.physics.montana.edu/winter/RSS_Presentation/SXT.ppt
Overview
Brief DescriptionThe Trouble with X-RaysOptical DesignSystem ParametersBlock DiagramEffective AreasWhy I Don’t Have a SNR Calculation NOBODY HAS A SNR CALCULATION !!!
Sample dataReferences
Soft X-Ray Telescope (SXT) was designed to study “thermal” X-ray emissions from solar coronal sources (1/2 MK-30 MK) 0.25 – 4 keV range (3-45 Å)
E[keV]=12.40[keV* Å]/[Å] Passive sensor
One of many instruments onboard Yohkoh Satellite
Launched from Kagoshima, Japan on August 31, 1991 Trae Winter arrives in Bozeman on January 6, 2002 to take
over MSU SXT science planning January 9, 2002 announced (to me at least) that Yohkoh was
lost on December 14, 2001.
Brief Description I
Brief Description II: SXT
http://isass1.solar.isas.ac.jp/yohkoh/images/teemsxt.gif
Brief Description III: Yohkoh (Solar-A)
Ogawara, Y., et al. 1991
Atmospheric transmission of X-Ray and E.U.V. is essentially 0 Sounding Rockets Satellites
X-Rays ignore “most” refractive optics The index of refraction, n[], is ~1 at X-ray
wavelengths for all material
X-Rays are not easily reflected More likely to be transmitted or absorbed
The Trouble withX-Rays I
X-Rays can be made to reflect off of high density materials at shallow angles Analogous to total internal reflection
critical is the angle in arcminutes, is the mass density in g cm-3, E is the photon energy in keV http://harris.roe.ac.uk/~jcm/thesis/thesis.html
The Trouble withX-Rays II
69.4critical E
Optical Design I:Wolter I Telescope
http://www.sr.bham.ac.uk/xmm/images/mirrors/lightanim.gif
Optical Design II:“Ray-Trace” of SXT (Mod. Wolter I)
http://www.lmsal.com/SXT/
Optical Design III:Breakaway
http://www.lmsal.com/SXT/
System ParametersCCD Cooled to ~-18°C Array Size:
1024 X 1024Pixel Size:18.281 0.002 m 2.4528 0.0005” 1779 km
Time Resolution:0.5 sec. (Special)2.0 sec. (normal)
TelescopeGeometrical Area261.75 mm2
Effective Area (Peak) 78 mm2 @ 8 ÅEffective Focal Length 1535.6 mm
ConstructionZerodur™ Glass/Ceramic420 Å Au on 80 Å CrSurface Roughness3.8 Å r.m.s.
Block DiagramMirror
FilterFilter CCD
Shutter
Data
Processor
Memory
10 MBGoldstone
Canberra
Madrid
Kagoshima
Effective Area I
Effective Area II:Now with filters
a) No filter
b)1265 Å Al
c) Dag
d)2.52 m Mg
e) 11.6 m Al
f) 119 m Be
SNR Calculation I
X
Energy Per [Å] CCD Response (e-/keV)
Sum the electons/s DN=(#E/100)+(13,30,69)
For noise repeat but the photon spectrum is now the square root of itself.
SNR Calculation IAssumptions
Solar active region
Electron Density 1 x 109 particles cm-
3
A certain set of elemental abundances
Ionization equilibrium approximations
SNR = 1.73 or 2.4 dB
Signal=22.5 DN s-1 pixel-1, Noise= 13 DN s-1 pixel-1
Why don’t I still have a true SNR??
Sample Data
Sample Data
http://www.lmsal.com/ypop/sxt_movie.html
ReferencesOgawara, Y., et al. 1991, “The Solar-A Mission - an Overview”, SOLAR PHYSICS, 136, pp. 1-16
Tsuneta, S., et al. 1991, “The Soft X-ray Telescope for the SOLAR-A Mission”, Solar Physics, 136, pp. 37-67
Web Resources:
Yohkoh Data Analysis Guide and Instrument Guide Available at
http://umbra.gsfc.nasa.gov/yohkoh_archive.html#YAG
ISAS Yohkoh Web Page
http://isass1.solar.isas.ac.jp/yohkoh/images/
James Manners’ Thesis Page
http://harris.roe.ac.uk/~jcm/thesis/thesis.html
Lockheed Martin Solar & Astrophysical Lab Yohkoh Web Page
http://www.lmsal.com/SXT/
Marshall Space Flight Center
http://science.nasa.gov/ssl/pad/solar/
Yohkoh Public Outreach Project
http://solar.physics.montana.edu/YPOP/
Slides that I deleted due to lack of time
Scientific Context:Begin the Space Age
“Almost” no E.U.V. or X-Ray photons @ surfaceNo reason to expect solar X-RaysSounding rockets detected X-RaysThen came OSO, SkylabRESOLUTION!!!
http://science.nasa.gov/ssl/pad/solar/images/s054_1.gifhttp://science.nasa.gov/ssl/pad/solar/images/skylab2.jpg
Temperature ResponseBased on synthetic spectra with certain input
parameters (elemental abundances, electron density, emission measure (amount of emitting plasma))